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      Fiber Optic Sensors for Structural Health Monitoring of Air Platforms

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          Abstract

          Aircraft operators are faced with increasing requirements to extend the service life of air platforms beyond their designed life cycles, resulting in heavy maintenance and inspection burdens as well as economic pressure. Structural health monitoring (SHM) based on advanced sensor technology is potentially a cost-effective approach to meet operational requirements, and to reduce maintenance costs. Fiber optic sensor technology is being developed to provide existing and future aircrafts with SHM capability due to its unique superior characteristics. This review paper covers the aerospace SHM requirements and an overview of the fiber optic sensor technologies. In particular, fiber Bragg grating (FBG) sensor technology is evaluated as the most promising tool for load monitoring and damage detection, the two critical SHM aspects of air platforms. At last, recommendations on the implementation and integration of FBG sensors into an SHM system are provided.

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          Most cited references72

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          Fiber Bragg grating technology fundamentals and overview

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            Fiber-Optic Sensing: A Historical Perspective

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              Development of smart composite structures with small-diameter fiber Bragg grating sensors for damage detection: Quantitative evaluation of delamination length in CFRP laminates using Lamb wave sensing

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                Author and article information

                Journal
                Sensors (Basel)
                Sensors (Basel, Switzerland)
                Molecular Diversity Preservation International (MDPI)
                1424-8220
                2011
                25 March 2011
                : 11
                : 4
                : 3687-3705
                Affiliations
                [1 ] Microwave Photonics Research Laboratory, School of Information Technology and Engineering, University of Ottawa, Ottawa, ON K1N 6N5, Canada; E-Mails: hguo062@ 123456uottawa.ca (H.G.); jpyao@ 123456site.uottawa.ca (J.Y.)
                [2 ] Institute for Microstructural Sciences, National Research Council Canada, Ottawa, ON K1A 0R6, Canada
                [3 ] Air Vehicles Research Section, Defence R&D Canada, Department of National Defence, National Defence Headquarters, Ottawa, ON K1A 0K2, Canada
                Author notes
                [* ]Authors to whom correspondence should be addressed; E-Mail: George.Xiao@ 123456nrc-cnrc.gc.ca (G.X.); Tel.: +1-613-991-6159 (G.X.); E-Mail: Nezih.Mrad@ 123456drdc-rddc.gc.ca (N.M.); Tel.: +1-613-993-6443 (N.M.).
                Article
                sensors-11-03687
                10.3390/s110403687
                3231328
                22163816
                e8343bb8-fb1b-4da1-bfad-1eb7f360d5a7
                © 2011 by the authors; licensee MDPI, Basel, Switzerland.

                This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution license ( http://creativecommons.org/licenses/by/3.0/).

                History
                : 1 February 2011
                : 18 March 2011
                : 21 March 2011
                Categories
                Review

                Biomedical engineering
                structural health monitoring,load monitoring,damage detection,fiber optic acoustic sensor,fiber bragg grating,aircraft

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